Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = '369D' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = '369D' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR 2006FA0001085Bearing · spalledVISIBLE LINE FOUND ON 2.5 BEARING ROLLERS MATCHING SPALLING FOUND ON SAG SHAFT (SDR DATED 3/NOV/2006). GEARBOX INSTALLED 6/SEPT/2006. TIME IN SERVICE FOR GEAR BOX, 105.1 HOURS. 2.5 BEARING INSTALLATION TIMES NUT SHOWN ON ENGINE CARDS. 2.5 BEARING IS A PMA SDR 2006FA0001086Support · corrodedDURING ANNUAL INSPECTION PEDAL SUPPORT WAS FOUND WITH CORROSION ON LOWER BOLT PADS BEYOND REPAIRABLE LIMITS. REPLACED SUPPORT BRACKET WITH SERVICEABLE PART. (K)SDR 2006FA0000959Gearbox · making metalFOUND PTO , PTO BALL BEARING AND TORQUEMETER SPALLED. FOUND CHIPS ON CHIP PLUGS. DISASSEMBLED GEAR BOX AND FOUND PTO GEAR, TORQUEMETER GEAR AND PTO BALL BEARING SPALLED. REPLACED GEARBOX. (K)SDR 2006FA0000958Turbine Wheel · damagedFOUND NR 1, AND NR 2 TURBINES RUBING AFTER ENGINE DISASSEMBLY FOR CHIPS. DURING 100 HR CHIPS WERE FOUND ON THE CHIP PLUGS. DISASSEMBLED ENGINE AND DISCOVERED THE N1 AND N2 TURBINES WERE RUBBING, REPLACED UNIT. (K)SDR 2006FA0000957Impeller · damagedDURING REPLACEMENT OF THE S16 SHAFT, IT WAS DISCOVERED THAT THE OUTER LAND OF THE SNAP RING GROOVE WAS VERY THIN AND THE INNER EDGE WAS LIFTING AND (2) .3750 INCH LONG PIECES CAME OFF OF THE LAND. WHEN THE SNAP RING WAS REMOVED THE GROVE FOR THE SNAP RING SESDR 2006FA0000948Case · erodedFOUND CASE HALVES SHOT. ENGINE RUNNING 35 DEGREES C, HOT. (K)SDR 2006FA0000947Combustion Case · crackedPILOT COMPLAINED THAT THE TOT SUDDENLY WENT 40 DEGREES C, HOT. FOUND OUTER COMBUSTION CAN CRACKS. REPLACED UNIT. (K)SDR CA060811002Belt · worn(CAN) ON APPROACH TO LAND THE PILOT HEARD A NOISE TO THE REAR OF THE AIRCRAFT FOLLOWED BY A VIBRATION. UPON INSPECTION THE ENGINEER NOTICED THE OIL COOLER BLOWER BELT TENSION WAS LOOSE AND THE TEETH OF THE BELT WERE WORN. (TC NR 20060811002)SDR CA060804010Bearing · cracked(CAN) 369D25146 ROLLER BEARING INNER RACE CRACKED, THIS RACE IS PRESSED ONTO TRANSMISSION T/R O/P PINION WITH AN INTERFERENCE FIT. CRACKED INNER RACE CAUSED THE RACE TO SPALL AND CAUSED A CHIP LIGHT. SEVERE METAL CONTAMINATION WAS FOUND (TC NR 20060804010)SDR CA060717008Window · detached(CAN) HELICOPTER WAS CLIMBING OUT AT 70 KTS WHEN THE RT FWD DOOR WINDOW IMPLODED INTO THE CABIN. UPON INVESTIGATION IT WAS FOUND THE WINDOW INSTALLED REQUIRED A RUBBER GASKET TO HOLD IT IN. THINKING IT WAS A MD WINDOW IT WAS INSTALLED WITH THE ORIGINAL FRAME.SDR CA060808009Strut · cracked(CAN) DURING THE YEARLY INSPECTION, THE LT AFT LANDING GEAR STRUT WAS INSPECTED AND FOUND TO BE CRACKED, FROM THE LOWER DRAG BRACE ATTACH HOLE. THE CRACK WAS APPROX. 1.250 INCH LONG, AND EXTENDED LENGTHWISE TOWARDS THE BEND IN THE STRUT (TC NR 20060808009)SDR CA060509007Strut · cracked(CAN) WHILE DOING A 100 HOUR INSPECTION OF THE AIRCRAFT THE ENGINEER NOTICED SOME CRACKED PAINT ON THE BOTTOM SIDE OF THE STRUT EMINATING FROM THE LANDING GEAR BRACE BOLT HOLE. HE THEN REMOVED SOME OF THE PAINT AND REVEALED A CRACK 1.5 INCHES LONG GOING OUTWASDR CA060320004Data Plate · loose(CAN) GLUE ON DATA TAG DETERIORATED DUE TO CONTACT WITH FUEL AND WAS LOCATED AT BOTTOM OF FUEL TANK (TC NR 20060320004)SDR CA060322009Belt · failed(CAN) DURING A 100 HOUR INSPECTION THE BLOWER BELT WAS NOTED AS HAVING SEVERAL TEETH MISSING. BELT IS IDENTIFED WITH THE PN IN WHITE MARKER. BELT TENSION WAS VERIFIED AFTER INSTALLATION AND NO DEFECTS WERE NOTED DURING THE NEXT 3-100 HOUR INSPECTIONS. NO VIBRASDR CA060220005Link · cracked(CAN) DURING A 100 HOUR INSPECTION THE ENGINEER NOTICED A CRACK ON ONE OF THE EARS OF THE LEAD LAG LINK OF THE MAIN ROTOR HUB ASSEMBLY. CRACK PROPAGATED FROM THE BUSHING OUTWARD. (TC NR 20060220005)SDR CA060208006Scroll · cracked(CAN) ON INSPECTION THE ENGINEER WAS TAKING APART THE ANTI-ICE BODY 6856984 FOR INSPECTION AND FOUND A CRACK AROUND THE BOSS. (TC NR 20060208006)SDR AU510002144Gearbox · making metal(AUS) TAIL ROTOR GEARBOX METAL CONTAMINATION. INVESTIGATION FOUND THE INPUT SHAFT REAR BEARING PN 369D25417 TO BE UNSERVICEABLE. INPUT SHAFT PN 369D25434 CRACKED IN AREA UNDER BEARING. (CASA NR 510002144)SDR CA051117004Mount Bracket · cracked(CAN) DURING SCHEDULED 300 HOUR AIRFRAME INSPECTION, A CRACK WAS FOUND IN THE COOLING FAN MOUNT. PART WAS REMOVED AND NEW PART WAS ORDERED ON MHI PO NR 204119. UNSERVICEABLE PART IS AVAILABLE IF REQUIRED. (TC 20051117004)SDR AOC05002Nozzle · departedUPON INSPECTION OF THE TURBINE ASSEMBLY, THE NOZZLE SHIELD DOME WAS FOUND TO BE COMPLETELY DETACHED FROM THE NOZZLE ASSEMBLY. APPEARS THAT NOZZLE SHIELD WAS NOT PROPERLY BRAZED IN PLACE AT MANUFACTURE. THIS NOZZLE ASSEMBLY NOT INCLUDED IN CEB-A-1370R2, WHICHSDR 2006FA0000113Line · leakingPILOT SAW TORQUE PRESS FLUCTUATE. TORQUE PRESS LINE TO GAUGE LEAKED AND ENGINE WAS STARVED OF OIL. THE AIRCRAFT HAD MADE A NORMAL LANDING AND SHUTOFF ENGINE SEIZED UP ON COASTDOWN, REPLACED ENGINE. (K)SDR 2005FA0001525Bracket · mismanufacturedRECEIVED A BLOWN BRACKET FROM THE VENDOR AND FOUND IT IS NOT BUILT TO THE LATEST SPECS, IT WAS BUILT IN 2002 AND REQUIRES MODIFICATIONS CALLED OUT IN AN SB. (K)SDR 2005FA0001523Stud · brokenFOUND THE LOWER RT COMPRESSOR STUD BROKEN OFF. DURING INSPECTION PROCESS FOR COMPRESSOR CASE HALVES. IT WAS NOTICED THAT THE RT LOWER COMPRESSOR STUD WAS MISSING (THAT IS THE NUT AND STUD WERE NOT VISABLE ON THE COMPRESSOR FLANGE). REPLACED UNIT. (K)SDR CA061002008Bearing · spalled(CAN) M/R TRANSMISSION CHIP DETECTOR FOUND TO HAVE A LARGE AMOUNT OF METAL. SOURCE FOUND TO BE THE T/R O/P PINION ROLLER BEARING INNER RACE. THE INNER RACE WAS FOUND TO HAVE HEAVY SPALLING IN A LARGE AREA. (APPROXIMATELY .550 INCH X .200 INCH) (TC NR 200610SDR CA050913011Bearing · unserviceable(CAN) ROD END BEARING WORN BEYOND SERVICEABLE LIMITS PREMATURELY. MANUFACTURER OF RODND BEARING, WARRANTY ON THIS BEARING AND PREVIOUS PREMATURELY WORN BEARINGS REJECTED. SUSPECT SUBSTANDARD PARTS DUE TO HIGH WEAR RATE, CONFIRMED BY OTHER OPERATORS.SDR 2005FA0001524Skid · crackedUPON LANDING THE MECHANIC SAW THE FORWARD LT SKID TUBE WAS ANGLED UP SEVERAL DEGREES. IT WAS DISCOVERED THAT THE TUBE WAS CRACKED UNDER THE FORWARD FOOT AND SKID PLATE. REPLACED UNIT. (K)SDR 2005FA0001320Bearing · failedENGINE CHIP LIGHTS FOLLOWED BY ENGINE NOISE. (K)SDR 2005FA0001336Governor · stiffON INSPECTION THE GOV LOOKED TO BE OUT OF RIG. WHEN THE ARM WAS REMOVED IT WAS DISCOVERED THAT THE SHAFT WAS EXTREMELY STIFF. REPLACED GOVERNOR. (K)SDR CA051123006Tip Cap · damaged(CAN) A/C HAD A BLADE REPLACED DUE TO A CRACK. NEW BLADE WAS VERY DIFFICULT TO BALANCE, SEEMED HEAVIER THAN THE OTHERS. BALANCING OF BLADES MET CRITERIA AND IT WAS RELEASED FOR SERVICE. SWEEPING OF BLADES WAS USELESS IN ACHIEVING BALANCE. SECOUND DAY OF THE JSDR 2005FA0001338Motor · inoperativePILOT BEEPED THE N2 UP AND WAS UNABLE TO BEAP DOWN, THEN LATER GOT IT DOWN WITH NUMEROUS ATTEMPTS AND FLEW IT BACK. UNIT WAS CHANGED. (K)SDR 2005FA0001339Hub · damagedFOUND THE UPPER M/R P/C LINK BEARING HAD WORN INTO THE ATTACH HUB OF THE PITCH HOUSING ABOUT .130 INCH UNTIL THE SPHERICAL PART OF THE BEARING CONTACTED, PREVENTING FURTHER PROGRESSION. (K)SDR CA050831002Blade · cracked(CAN) DURING PILOT'S POST FLIGHT INSPECTION A CRACK WAS DETECTED IN THE LOWER SKIN OF MAIN ROTOR BLADE NR 1. THE CRACK IS LOCATED 11' FROM THE INBOARD END (ROOT FITTING) OF THE BLADE, AND 3' AFT OF THE LEADING EDGE. THE CRACK WAS 3' LONG AND WITHIN 1' OF THESDR CA051117006Blade · cracked(CAN) DURING TRAINING FOR TORQUE EVENT INSPECTION (AWD2003-24-01) A POSSIBLE CRACK WAS FOUND. THE M/R BLADE WAS REMOVED FOR A BETTER VISUAL LOOK WITH THE 10X GLASS. THE BLADE WAS ALSO INSPECTED BY COUGAR NDE LTD. AND CONFIRMED THE CRACK. MHI PO NR 20385. TSDR CA050913010Bearing · unserviceable(CAN) ROD END BEARING WORN BEYOND SERVICEABLE LIMITS PREMATURELY. MANUFACTURER OF RODEND BEARING. WARRANTY ON THIS BEARING AND PREVIOUS PREMATURELY WORN BEARINGS REJECTED. SUSPECT SUBSTANDARD PARTS DUE TO HIGH WEAR RATE, CONFIRMED BY OTHER OPERATORS.SDR 2005FA0001052Transmission · unserviceableDURING ROTATION OF THE M/R HUB WHILE PERFORMING ROUTINE MAINTENANCE A NOTICEABLE (SQUEAK) WAS HEARD COMING FROM THE M/R TRANSMISSION. SUBSEQUENT INVESTIGATION ALLOWED FOR THE DISCOVERY OF THE INPUT PINION HAVING SIDE SLOPE AND THE SQUEAK WAS HEARD WITH A LISTSDR CA050503015Blade · cracked(CAN) CRACK FOUND DURING M/R BLADE TORQUE EVENT INSP. CRACK IS APPROX. 11 INCHES OUT FROM BLADE GRIP ON LOWER SURFACE OF BLADE. CRACK RUNS CORDWISE AND IS APPROX. 3.5INCHES LONG.SDR AOC05001Swashplate · misinstalledWHEN REPLACING THE SWASHPLATE ASSEMBLY. IT WAS NOTED THAT MASTINOX WAS USED INSTEAD OF MIL-P-85582 AS REQUIRED BY THE MANUFACTURES MAINTENANCE MANUAL. USE OF MASTINOX WILL ALLOW THE UNIBALL TO ROTATE IN THE SWASHPLATE. WHEN THE MAINTENANCE FACILITY WAS CONTASDR CA050414002Gear · brokenMAIN ROTOR TRANSIMISSION SENT IN FOR REPAIR DUE TO REPORTED CHIPS ON DETECTOR. TRANSIMISSION OPENED AND APPROXIMATELY 2/3 OF TOOTH (CENTER PORTION) FOUND MISSING FROM INPUT GEAR. PIECE LOCATED INSIDE TRANSIMISSION CASE. NO FURTHER DAMAGE NOTED.SDR CA050414003Gear · brokenMAIN ROTOR TRANSMISSION SENT IN FOR REPAIR DUE TO REPORTED CHIPS ON DETECTOR. TRANSMISSION OPENED AND APPR NR 2/3 OF TOOTH (CENTER PORTION) FOUND MISSING FROM INPUT GEAR. PIECE LOCATED INSIDE TRANSMISSION CASE. NO FURTHER DAMAGE NOTED.SDR CA050329015Safety Valve · broken(CAN) AERONAUTICAL ACCESSORIES PC SAFETY VALVE KIT, STC SE327AT, STA SE93-4. UPON REMOVAL FOR OVERHAUL THE ACTUATING KNOB WAS FOUND SHEARED AND HELD IN PLACE BY THE RETAINING CLIP. THE KNOB WOULD NOT HAVE FALLEN HOWEVER THE VALVE ITSELF WAS NO LONGER HELD IN SDR CA050306001Blade · cracked(CAN) MAIN ROTOR BLADE SKIN CRACKED AT DOUBLER LIP ON BOTTOM SIDE OF BLADE CHORDWISE. CRACK LENGTH 2 INCHES. RUNS UNDERNEATH SEALANT THAT BOND DOUBLER TO THE BLADE. FOUND DURING 100 HR INSPECTION M/R TORQUE EVENT INSPECTION.SDR CA050215006Coupling · undersize(CAN) UPON INSPECTION BEFORE BEING ENTERED INTO STORES IT WAS NOTED THAT THE BOLT HOLES WERE UNDERSIZE. THE COUPLING HAS BEEN RETURNED TO THE PARTS SUPPLIER.SDR 2004FA0000926Cyclic Stick · looseDURING ANNUAL INSPECTION IT WAS DISCOVERED THAT THE CYCLIC STICK HAD ABOUT HALF FORE AND AFT PLAY CAUSED BY A LOOSE FIT AT THE CYCLIC PIVOT POINT AT THE CYCLIC TORQUE TUBE. WHEN IT WAS DISASSEMBLED IT WAS FOUND TO HAVE BEEN SHIMMED WITH COMPRESSOR SHIMS WHICHSDR 2004FA0000924Torque Tube · out of limitsFOUND AN AREA ON THE T/R PEDAL TORQUE TUBE THAT WAS DRESSED OUT WAY BEYOND LIMITS NEARLY HALF THE WALL THICKNESS AND THE AREA NOTED COULD NOT BE SEEN CLEARLY UNTILL IT WAS DISASSEMBLED. REPLACED TUBE.SDR CA041112005Sprag Clutch · broken(CAN) CLUTCH REMOVED FOR GREASE BEARING REPLACEMENT. UPON INSPECTION 2 SPRAGS FOUND BROKEN.SDR 2005FA0000434Engine · making metalPILOT HAD ENGINE CHIP LIGHT ILLUMINATION FOLLOWED ALMOST IMMEDIATELY WITH A NOISE/VIBRATION, THEN A POWER LOSS/ DECEL. AC LANDED WITHOUT INCIDENT AND PILOT HAD TO SHUT OFF THE ENGINE. CHIP PLUGS AND OIL FILTERS WERE CONTAMINATED WITH METAL. DISASSEMBLY OF ESDR CA041026011Transmission · corroded(CAN) SEVERE CORROSION FOUND IN OIL GALLERY BEHIND M/R XMSN UPPER BEARING LINER FOR 369D25149 AND 369D25148 BEARINGS. PROBLEM INITIALLY INDICATED BY LACK OF FLOW FROM OIL ORFICES. CORROSION FOUND BY REWORK FACILITY DURING LINER REMOVAL, AND WAS UNDETECTABLE SDR CA041013006Blade · cracked(CAN) HELICOPTER WAS FLYING WITH EXTERNAL LOAD WHEN THE PILOT FELT A (BUMP) IN THE CONTROLS. THE WEATHER WAS DETERIOATING WHERE HE WAS OPERATING SO HE RETURNED TO THE STAGING AREA. THE PILOT INSPECTED THE BLADES AFTER SHUTDOWN AND FOUND A 4.5 INCH CRACK 19 INCSDR NM09EDR001Mast · corrodedDURING 100 HR INSPECTION, THE MAIN ROTOR DRIVESHAFT WAS REMOVED FOR INSPECTION. THE MECHANIC LOOKED DOWN THE MAST AND FOUND THE PAINT ON THE INSIDE DIAMETER WAS BLISTERED AND PEELING. THE MECHANIC ALSO NOTICED PAINT ON THE TOP OF THE MAIN TRANSMISSION SPLINES.SDR CA040825013Shaft · broken(CAN) PILOT REPORTED THAT WHEN DESCENDING RAPIDLY, COLLECTIVE BOTTOMED OUT AND RT PEDAL INPUT, THE PEDALS WOULD VIBRATE AND THE AIRFRAME WOULD VIBRATE AND WITH A LITTLE COLLECTIVE INPUT AND LT PEDAL THE VIBRATION WOULD GO AWAY. THE SAME COULD BE INDUCED ON THESDR HXSD2004802Gearbox · making metalPILOT REPORTED A CHIP LIGHT FOR THE TAIL ROTOR GEAR BOX. MECHANIC INVESTIGATED AND FOUND FOUR HAIR LINE SLIVERS ON THE CHIP PLUG ALL WHICH EXCEEDED LIMITS AS DESCRIBED BY THE MM. REMOVED THE GEAR BOX (PN 369D25400 SN 0295) AND INSTALLED SERVICEABLE GEAR BOX
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